AER 320 - PROPULSION

College of Engineering

Credit(s): 3

This course examines the theory and fundamentals of cycle analysis for aerospace systems including gas-turbine engine power cycles and rocket engine systems. Fundamentals of combustion are covered including chemical equilibrium, adiabatic flame temperature and heat release. Introduction to fluid analysis for turbomachinery and alternative propulsion systems is included.

Prereq: AER/ME 220, MA 214 and Engineering Standing.